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Interference of Wing and Fuselage From Tests of the 18 Combinations in the N.A.C.A. Variable-Density Tunnel - Combination With Split Flaps
Author:
Sherman, Albert
Year:
1938
Document Type:
N/A
Series:
NACA Technical Notes
Report Number:
NACA-TN-640
Link:
https://digital.library.unt.edu/ark:/67531/metadc54523/
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